Gracey, M.W. and Galbraith, R.A.M. (1989) Data for a NACA 23012C Aerofoil Pitched about its Quarter Chord Axis. Volume II: Pressure Data from Oscillatory Tests. G.U. Aero report 8902. Technical Report. Department of Aerospace Engineering, University of Glasgow.
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Text (scanned version of the original print report)
183858.pdf - Published Version 125MB |
Abstract
Herein is presented the collected data for tests in which a NACA 23012C aerofoil was subjected to a variety of oscillatory type displacements in pitch about the quarter chord position at low Reynolds numbers.
| Item Type: | Research Reports or Papers (Technical Report) |
|---|---|
| Additional Information: | "NACA 23012C - VOLUME II": at head of title page. |
| Status: | Published |
| Glasgow Author(s) Enlighten ID: | Galbraith, Professor Roderick |
| Authors: | Gracey, M.W., and Galbraith, R.A.M. |
| College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
| Publisher: | Department of Aerospace Engineering, University of Glasgow |
| Copyright Holders: | Copyright © 1989 Department of Aerospace Engineering, University of Glasgow |
| Publisher Policy: | Reproduced with the permission of the Department |
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